View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 17528U 26042.01133034 +.00000000 +00000-0 +14850-3 0 00006
2 17528 97.4026 50.6013 0145910 97.2670 264.5140 14.54431842 07
| Epoch (UTC): | 11 February 2026 00:16:18 |
| Eccentricity: | 0.0145910 |
| inclination: | 97.4026° |
| perigee height: | 608 km |
| apogee height: | 815 km |
| right ascension of ascending node: | 50.6013° |
| argument of perigee: | 97.2670° |
| revolutions per day: | 14.54431842 |
| mean anomaly at epoch: | 264.5140° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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